RAE 5214 AIRFOIL (rae5214-il)
RAE 5214 AIRFOIL - RAE 5214 transonic airfoil
| Details | Dat file | Parser | |
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(rae5214-il) RAE 5214 AIRFOIL RAE 5214 transonic airfoil Max thickness 9.7% at 35.5% chord. Max camber 1.4% at 69.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
RAE 5214 AIRFOIL
42. 42.
0.00000 0.00000
0.00050 0.00522
0.00100 0.00732
0.00160 0.00925
0.00241 0.01128
0.00350 0.01343
0.00500 0.01580
0.00650 0.01778
0.00800 0.01940
0.00961 0.02090
0.01500 0.02480
0.02153 0.02841
0.03000 0.03216
0.03806 0.03496
0.05904 0.04029
0.08427 0.04434
0.11349 0.04776
0.14645 0.05045
0.18280 0.05276
0.22221 0.05480
0.26430 0.05640
0.30866 0.05744
0.35486 0.05778
0.40245 0.05742
0.45099 0.05642
0.50000 0.05478
0.54901 0.05234
0.59755 0.04917
0.64514 0.04524
0.69134 0.04071
0.73570 0.03586
0.77779 0.03082
0.81720 0.02581
0.85355 0.02094
0.88651 0.01641
0.91573 0.01236
0.94096 0.00870
0.96194 0.00562
0.97847 0.00302
0.99039 0.00133
0.99759 0.00034
1.00000 0.00000
0.00000 0.00000
0.00050 -0.00410
0.00100 -0.00545
0.00160 -0.00665
0.00241 -0.00785
0.00350 -0.00900
0.00500 -0.01030
0.00650 -0.01139
0.00800 -0.01228
0.00961 -0.01316
0.01500 -0.01533
0.02153 -0.01727
0.03000 -0.01947
0.03806 -0.02118
0.05904 -0.02459
0.08427 -0.02786
0.11349 -0.03074
0.14645 -0.03332
0.18280 -0.03556
0.22221 -0.03731
0.26430 -0.03856
0.30866 -0.03915
0.35486 -0.03889
0.40245 -0.03773
0.45099 -0.03560
0.50000 -0.03232
0.54901 -0.02788
0.59755 -0.02267
0.64514 -0.01716
0.69134 -0.01199
0.73570 -0.00768
0.77779 -0.00424
0.81720 -0.00175
0.85355 -0.00010
0.88651 0.00085
0.91573 0.00130
0.94096 0.00126
0.96194 0.00098
0.97847 0.00062
0.99039 0.00029
0.99759 0.00006
1.00000 0.00000
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Polars for RAE 5214 AIRFOIL (rae5214-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| rae5214-il | 50,000 | 9 | 29.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 50,000 | 5 | 27.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5214-il | 100,000 | 9 | 40.3 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 100,000 | 5 | 35.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5214-il | 200,000 | 9 | 46.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 200,000 | 5 | 49.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5214-il | 500,000 | 9 | 66.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 500,000 | 5 | 68.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rae5214-il | 1,000,000 | 9 | 83.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rae5214-il | 1,000,000 | 5 | 80.7 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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